Helicopter main reducer fairing locking reliability inspection tool
The utility model belongs to the technical field of displacement measurement, and particularly relates to a helicopter main speed reducer fairing locking reliability inspection tool, which comprises a sleeve, a measuring rod and an indication assembly, a piston is arranged at one end of the measurin...
Gespeichert in:
| Hauptverfasser: | , , , , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | LI XIAOYAN JIANG DONGLIANG ZHU XUNKE YUAN KAI MA YI JIANG YONGNING SU SHIWEI ZHANG QIANG LIU FANGMING CHEN CHUNYUAN |
| description | The utility model belongs to the technical field of displacement measurement, and particularly relates to a helicopter main speed reducer fairing locking reliability inspection tool, which comprises a sleeve, a measuring rod and an indication assembly, a piston is arranged at one end of the measuring rod, a sliding hole is arranged in the sleeve, the piston slides close to the sliding hole, and the measuring rod can extend out of the sleeve; the inner wall of the sliding hole is connected with the piston through a spring; a mounting groove is formed in the side wall of the sleeve, the mounting groove is communicated with the sliding hole, and a graduated scale is arranged on the mounting groove; the indicating assembly comprises a sliding part and an indicating scale arranged on the sliding part, the sliding part is arranged in a sliding mode close to the sliding hole, and the indicating end of the indicating scale is arranged right opposite to the graduated scale. The tool can quickly complete the length mea |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN220625121UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN220625121UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN220625121UU3</originalsourceid><addsrcrecordid>eNrjZHD2SM3JTM4vKEktUshNzMxTKEpNKU0GctISM4sy89IVcvKTs0F0EVBdYlJmTmZJpUJmXnFBanJJZn6eQkl-fg4PA2taYk5xKi-U5mZQcnMNcfbQTS3Ij08tLkhMTs1LLYl39jMyMjAzMjU0MgwNNSZKEQAlfzPB</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Helicopter main reducer fairing locking reliability inspection tool</title><source>esp@cenet</source><creator>LI XIAOYAN ; JIANG DONGLIANG ; ZHU XUNKE ; YUAN KAI ; MA YI ; JIANG YONGNING ; SU SHIWEI ; ZHANG QIANG ; LIU FANGMING ; CHEN CHUNYUAN</creator><creatorcontrib>LI XIAOYAN ; JIANG DONGLIANG ; ZHU XUNKE ; YUAN KAI ; MA YI ; JIANG YONGNING ; SU SHIWEI ; ZHANG QIANG ; LIU FANGMING ; CHEN CHUNYUAN</creatorcontrib><description>The utility model belongs to the technical field of displacement measurement, and particularly relates to a helicopter main speed reducer fairing locking reliability inspection tool, which comprises a sleeve, a measuring rod and an indication assembly, a piston is arranged at one end of the measuring rod, a sliding hole is arranged in the sleeve, the piston slides close to the sliding hole, and the measuring rod can extend out of the sleeve; the inner wall of the sliding hole is connected with the piston through a spring; a mounting groove is formed in the side wall of the sleeve, the mounting groove is communicated with the sliding hole, and a graduated scale is arranged on the mounting groove; the indicating assembly comprises a sliding part and an indicating scale arranged on the sliding part, the sliding part is arranged in a sliding mode close to the sliding hole, and the indicating end of the indicating scale is arranged right opposite to the graduated scale. The tool can quickly complete the length mea</description><language>chi ; eng</language><subject>MEASURING ; MEASURING ANGLES ; MEASURING AREAS ; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS ; MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS ; PHYSICS ; TESTING</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240319&DB=EPODOC&CC=CN&NR=220625121U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240319&DB=EPODOC&CC=CN&NR=220625121U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LI XIAOYAN</creatorcontrib><creatorcontrib>JIANG DONGLIANG</creatorcontrib><creatorcontrib>ZHU XUNKE</creatorcontrib><creatorcontrib>YUAN KAI</creatorcontrib><creatorcontrib>MA YI</creatorcontrib><creatorcontrib>JIANG YONGNING</creatorcontrib><creatorcontrib>SU SHIWEI</creatorcontrib><creatorcontrib>ZHANG QIANG</creatorcontrib><creatorcontrib>LIU FANGMING</creatorcontrib><creatorcontrib>CHEN CHUNYUAN</creatorcontrib><title>Helicopter main reducer fairing locking reliability inspection tool</title><description>The utility model belongs to the technical field of displacement measurement, and particularly relates to a helicopter main speed reducer fairing locking reliability inspection tool, which comprises a sleeve, a measuring rod and an indication assembly, a piston is arranged at one end of the measuring rod, a sliding hole is arranged in the sleeve, the piston slides close to the sliding hole, and the measuring rod can extend out of the sleeve; the inner wall of the sliding hole is connected with the piston through a spring; a mounting groove is formed in the side wall of the sleeve, the mounting groove is communicated with the sliding hole, and a graduated scale is arranged on the mounting groove; the indicating assembly comprises a sliding part and an indicating scale arranged on the sliding part, the sliding part is arranged in a sliding mode close to the sliding hole, and the indicating end of the indicating scale is arranged right opposite to the graduated scale. The tool can quickly complete the length mea</description><subject>MEASURING</subject><subject>MEASURING ANGLES</subject><subject>MEASURING AREAS</subject><subject>MEASURING IRREGULARITIES OF SURFACES OR CONTOURS</subject><subject>MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS</subject><subject>PHYSICS</subject><subject>TESTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHD2SM3JTM4vKEktUshNzMxTKEpNKU0GctISM4sy89IVcvKTs0F0EVBdYlJmTmZJpUJmXnFBanJJZn6eQkl-fg4PA2taYk5xKi-U5mZQcnMNcfbQTS3Ij08tLkhMTs1LLYl39jMyMjAzMjU0MgwNNSZKEQAlfzPB</recordid><startdate>20240319</startdate><enddate>20240319</enddate><creator>LI XIAOYAN</creator><creator>JIANG DONGLIANG</creator><creator>ZHU XUNKE</creator><creator>YUAN KAI</creator><creator>MA YI</creator><creator>JIANG YONGNING</creator><creator>SU SHIWEI</creator><creator>ZHANG QIANG</creator><creator>LIU FANGMING</creator><creator>CHEN CHUNYUAN</creator><scope>EVB</scope></search><sort><creationdate>20240319</creationdate><title>Helicopter main reducer fairing locking reliability inspection tool</title><author>LI XIAOYAN ; JIANG DONGLIANG ; ZHU XUNKE ; YUAN KAI ; MA YI ; JIANG YONGNING ; SU SHIWEI ; ZHANG QIANG ; LIU FANGMING ; CHEN CHUNYUAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN220625121UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>MEASURING</topic><topic>MEASURING ANGLES</topic><topic>MEASURING AREAS</topic><topic>MEASURING IRREGULARITIES OF SURFACES OR CONTOURS</topic><topic>MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS</topic><topic>PHYSICS</topic><topic>TESTING</topic><toplevel>online_resources</toplevel><creatorcontrib>LI XIAOYAN</creatorcontrib><creatorcontrib>JIANG DONGLIANG</creatorcontrib><creatorcontrib>ZHU XUNKE</creatorcontrib><creatorcontrib>YUAN KAI</creatorcontrib><creatorcontrib>MA YI</creatorcontrib><creatorcontrib>JIANG YONGNING</creatorcontrib><creatorcontrib>SU SHIWEI</creatorcontrib><creatorcontrib>ZHANG QIANG</creatorcontrib><creatorcontrib>LIU FANGMING</creatorcontrib><creatorcontrib>CHEN CHUNYUAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LI XIAOYAN</au><au>JIANG DONGLIANG</au><au>ZHU XUNKE</au><au>YUAN KAI</au><au>MA YI</au><au>JIANG YONGNING</au><au>SU SHIWEI</au><au>ZHANG QIANG</au><au>LIU FANGMING</au><au>CHEN CHUNYUAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Helicopter main reducer fairing locking reliability inspection tool</title><date>2024-03-19</date><risdate>2024</risdate><abstract>The utility model belongs to the technical field of displacement measurement, and particularly relates to a helicopter main speed reducer fairing locking reliability inspection tool, which comprises a sleeve, a measuring rod and an indication assembly, a piston is arranged at one end of the measuring rod, a sliding hole is arranged in the sleeve, the piston slides close to the sliding hole, and the measuring rod can extend out of the sleeve; the inner wall of the sliding hole is connected with the piston through a spring; a mounting groove is formed in the side wall of the sleeve, the mounting groove is communicated with the sliding hole, and a graduated scale is arranged on the mounting groove; the indicating assembly comprises a sliding part and an indicating scale arranged on the sliding part, the sliding part is arranged in a sliding mode close to the sliding hole, and the indicating end of the indicating scale is arranged right opposite to the graduated scale. The tool can quickly complete the length mea</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN220625121UU |
| source | esp@cenet |
| subjects | MEASURING MEASURING ANGLES MEASURING AREAS MEASURING IRREGULARITIES OF SURFACES OR CONTOURS MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS PHYSICS TESTING |
| title | Helicopter main reducer fairing locking reliability inspection tool |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-20T15%3A34%3A58IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=LI%20XIAOYAN&rft.date=2024-03-19&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN220625121UU%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |